The performance of composite repairing using single lapped joints is sensit
ive to factors such as ply stacking sequence of laminate, bonding surface p
reparation, anisotropic nature of adherend, as well as bearing and load tra
nsfer from one adherend to the other.
This research is focused to investigate the stress distributions in laminat
ed composite joints with multiple pin loads using finite element analysis.
The structural response of various configurations of single lap joints, nam
ely bonded, bolted and bonded-bolted joints, are analyzed by three-dimensio
nal finite element method.
A comparison of the results obtained using finite element analysis is condu
cted with experimental results and the results are validated. Parametric st
udy is conducted to investigate the effect of stress distribution and load
transfer due to ply stacking sequence of laminate.